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A high efficiency laminar flow burner system for proving a stream of heat energy including a supply input module for providing fuel and laminar streams of air to a combustion manifold. The combustion manifold includes an air-fuel mixing system, a stoichiometric unit, and a refractory unit each coupl

A high efficiency laminar flow burner system for proving a stream of heat energy including a supply input module for providing fuel and laminar streams of air to a combustion manifold. The combustion manifold includes an air-fuel mixing system, a stoichiometric unit, and a refractory unit each coupled to one another. A first combustion stream is established at the air-fuel mixing chamber system as fuel exits an injector device at direction perpendicular to the laminar air intake stream. A laminar air intake stream traveling from the supply input module and along the staging passageway passes through a stoichiometric unit body at a plurality of air intakes to meet with the first combustion stream within to define a second combustion stream for introduction from the stoichiometric unit to the refractory unit. The refractory unit thus defines a third combustion stream as the second combustion stream travels across a refractory passageway.

대표청구항 ▼

1. A laminar burner system comprising: a laminar air delivery system, the laminar air delivery system including a damper, a blower, and an air feed line, the damper directly receives atmospheric air and provides the collected atmospheric air to the blower coupled to the damper;a supply input module,

1. A laminar burner system comprising: a laminar air delivery system, the laminar air delivery system including a damper, a blower, and an air feed line, the damper directly receives atmospheric air and provides the collected atmospheric air to the blower coupled to the damper;a supply input module, the supply input module is coupled to the air feed line, the blower accelerates the air out the blower toward the supply input module;a combustion manifold, the combustion manifold in fluid communication with the supply input module; the air feed line establishes at least one laminar air flow stream for use with a combustion process applied within the combustion manifold,the supply input module providing a fuel and a laminar air intake stream to the combustion manifold, the combustion manifold includesan air-fuel mixing chamber system, the air-fuel mixing chamber system in fluid communication with the supply input module, and includes a mixing chamber and an injector device extending within the mixing chamber and along an alignment axis that extends through the combustion manifold, whereby fuel exits the injector device perpendicular to the laminar air intake stream traveling along the air-fuel mixing chamber system to combine to define a first combustion stream that flows along the alignment axis,a stoichiometric combustion unit, the stoichiometric combustion unit in fluid communication with the supply input module and the air-fuel mixing chamber system, includes a staging passageway and a stoichiometric unit body, the stoichiometric body includes a central axis that is defined by the alignment axis, the stoichiometric unit body extending along the central axis as well as a mixing plate and a stoichiometric plate, each transversely fixed to each end of the stoichiometric unit body, the stoichiometric unit body defines a plurality of air intakes, the plurality of air intakes pass through the stoichiometric unit body, whereby the laminar air intake stream traveling along the staging passageway passes through the plurality of air intakes so as to enter a hollow of the stoichiometric unit body to transversely intersect and combine with the first combustion stream that flows parallel to the alignment axis within the hollow of the stoichiometric unit body to define a second combustion stream that flows along the alignment axis; anda refractory unit, the refractory unit in fluid communication with the stoichiometric combustion unit, the refractory unit includes a refractory unit body, the refectory unit body defining a conically shaped refractory passageway with the vertex of the cone shape emerging from the stoichiometric body and expanding outwardly through the refractory unit body, the refractory unit passageway, in fluid communication with the stoichiometric unit body, receives the second combustion stream to define a third combustion stream formed within the refractory unit passageway, the refractory passageway maintains continuous laminar air flow through the combustion manifold; andan alignment plate, the alignment plate is coupled between the laminar air delivery system and the combustion manifold, the alignment plate in fluid communication with the laminar air delivery system and the combustion manifold the alignment plate defines the alignment axis, the alignment axis defines the centerline for both the injector device and the alignment plate, the alignment axis is a spatial reference for orienting ejected fuel from the injector device as the ejected fuel combines with the perpendicularly flowing laminar air intake stream, the alignment plate defines a portion of the mixing chamber, the injector device extends within the mixing chamber and outwardly from the alignment plate, along the alignment axis, to establish positive air pressure within the mixing chamber such that fuel exits the injector device perpendicular to the laminar air intake stream traveling along the air-fuel mixing chamber system to define the first combustion stream, first combustion stream flows parallel to the alignment axis, the alignment plate defines a plurality of inlet ports configured to receive air from the air feed line of the laminar air delivery system, a sealing door slideably contacts an inlet port of the plurality of inlet ports to variably expose the corresponding inlet port between a closed position and an open position to variably control the flow rate of the laminar air intake stream. 2. The laminar burner system according to claim 1 wherein the damper selectively provides the collected atmospheric air to the blower coupled to the damper. 3. The laminar burner system according to claim 1 wherein the damper selectively provides air to the combustion manifold coupled to the damper. 4. The laminar burner system according to claim 1 wherein the refractory unit releasably couples to and is in fluid communication with the energy consumption system. 5. The laminar burner system according to claim 1 wherein the air-fuel mixing chamber system includes a pilot unit disposed adjacent to the injector, the pilot unit including a variable resistor receiving a voltage for selective engagement of the pilot unit. 6. The laminar burner system according to claim 1 wherein the plurality of inlet ports receive the air from the feed line to establish laminar fluid flow thereto and continuously supply at least one laminar air intake stream to the combustion manifold. 7. A laminar burner system comprising: a laminar air delivery system, the laminar air delivery system including a damper, a blower, and air delivery line, and an air feed line, the damper is disposed on one distal end of the delivery line, the blower directly receives atmospheric air and provides the collected atmospheric air from the damper to the blower, the air feed line establishes, in part, a laminar air flow stream between the blower and the combustion manifold; a supply input module, the supply input module is coupled to the air feed line, the blower accelerates the air out the blower toward the supply input module; a combustion manifold, the combustion manifold in fluid communication with the supply input module; the air feed line establishes at least one laminar air flow stream for use with the combustion process applied with the combustion manifold, the supply input module providing a fuel and a laminar air intake stream to the combustion manifold, the combustion manifold includes an air-fuel mixing chamber system, the air-fuel mixing chamber system in fluid communication with the supply input module, and includes a mixing chamber and an injector device extending with the mixing chamber, whereby fuel exits the injector device to mix with the laminar air intake stream traveling along the air-fuel mixing chamber to define a first combustion stream, and includes a mixing chamber and an injector device extending within the mixing chamber and along an alignment axis that extends through the combustion manifold, whereby fuel exits the injector device perpendicular to the laminar air intake stream traveling along the air-fuel mixing chamber system to combine to define a first combustion stream that flows along the alignment axis, a stoichiometric combustion unit, the stoichiometric combustion unit in fluid communication with the supply input module and the air-fuel mixing chamber system, and includes a staging passageway and a stoichiometric unit body, the stoichiometric body includes a central axis that is defined by the alignment axis, the stoichiometric unit body extending along the central axis as well as a mixing plate and a stoichiometric plate, each transversely fixed to each end of the stoichiometric unit body, the stoichiometric unit body defines a plurality of air intakes, the plurality of air intake pass through the stoichiometric unit body, whereby the laminar air intake stream traveling along the staging passageway passes through the plurality of air intakes so as to enter a hollow of the stoichiometric unit body to transversely intersect and combine with the first combustion stream that flows parallel to the alignment axis within the hollow of the stoichiometric unit body to define a second combustion stream that flows along the alignment axis; and a refractory unit, the refractory unit in fluid communication with the stoichiometric combustion unit, the refractory unit includes a refractory unit body, the refrectory unit body defining a conically shaped refractory passageway with the vertex of the cone shape emerging from the interface with the stoichiometric body and expanding outwardly through the refractory unit body, the refractory unit passageway, in fluid communication with the stoichiometric unit body, receives he second combustion stream to define a third combustion stream formed within the refractory unit passageway, the refractory passageway maintains continuous laminar air flow through the combustion manifold; and an alignment plate, the alignment plate is coupled between the laminar air delivery system and the combustion manifold, the alignment plate in fluid communication with the laminar air delivery system and the combustion manifold the alignment plate defines the alignment plate, the alignment axis defines the centerline for both the injector device and the alignment plate, the alignment axis is a spatial reference for orienting ejected fuel from the injector device as the ejected fuel combines with the perpendicularly flowing laminar air intake stream, the alignment plate defines a portion of the mixing chamber, the injector device extends within the mixing chamber and outwardly from the alignment plate, along the alignment axis, to establish positive air pressure within the mixing chamber such that fuel exits the injector device perpendicular to the laminar air intake stream traveling along the air fuel mixing chamber system to define the first combustion stream, first combustion stream flows parallel to the alignment axis, the alignment plate defines a plurality of inlet ports configured to receive air from the air feed line of the laminar air delivery system, a sealing door slideably contacts an inlet port of the plurality of inlet ports to variably expose the corresponding inlet port between a closed position and an open position to variably control the flow rate of the laminar air intake stream. 8. The laminar burner system according to claim 7 wherein the damper controls the flow of atmospheric air to the blower.